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Simulating Rocket Trajectory Using JSBSim and Optimal Thrust Profile for maximizing altitude of sounding rocket

Simulating Rocket Trajectory Using JSBSim and Optimal Thrust Profile for maximizing altitude of sounding rocket

Celal Bayar Üniversitesi Fen Bilimleri Dergisi

2022-Cilt: 18 - Sayı: 4

417-424

Flight Simulator, JSBSim, Optimization, Sounding Rocket, Thrust-Time Profile

3217

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